test_cold_gas_thruster.TestSolvedChambertPlotPath Class Reference

Public Member Functions
	test_solved_path_selected (self)
	test_contour_shape (self)
	test_contour_starts_at_chamber_radius (self)
	test_contour_ends_at_exit_radius (self)
	test_contour_has_throat (self)
	test_contour_throat_smaller_than_chamber (self)
	test_lstar_auto_computed (self)
	test_lstar_explicit (self)

Detailed Description

Verify generate_nozzle_contour() works correctly via solved_chamber_plot.

Definition at line 218 of file test_cold_gas_thruster.py.

Member Function Documentation

test_contour_ends_at_exit_radius()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_contour_ends_at_exit_radius

(

self

)

Definition at line 238 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

test_contour_has_throat()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_contour_has_throat

(

self

)

Minimum radius in the contour should be ~= throat radius.

Definition at line 244 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

test_contour_shape()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_contour_shape

(

self

)

Definition at line 225 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

test_contour_starts_at_chamber_radius()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_contour_starts_at_chamber_radius

(

self

)

Definition at line 232 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

test_contour_throat_smaller_than_chamber()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_contour_throat_smaller_than_chamber

(

self

)

Definition at line 252 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

test_lstar_auto_computed()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_lstar_auto_computed

(

self

)

If Lstar=0, it should be computed from volume/A_throat without error.

Definition at line 258 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

test_lstar_explicit()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_lstar_explicit

(

self

)

Providing an explicit Lstar should also work without error.

Definition at line 265 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

test_solved_path_selected()

test_cold_gas_thruster.TestSolvedChambertPlotPath.test_solved_path_selected

(

self

)

Definition at line 221 of file test_cold_gas_thruster.py.

References test_cold_gas_thruster._make_solved_config().

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The documentation for this class was generated from the following file:

• EngineDesign/tests/test_cold_gas_thruster.py